亚洲免费av电影一区二区三区,日韩爱爱视频,51精品视频一区二区三区,91视频爱爱,日韩欧美在线播放视频,中文字幕少妇AV,亚洲电影中文字幕,久久久久亚洲av成人网址,久久综合视频网站,国产在线不卡免费播放

        ?

        Updating empirical results of wind loads on cooling towers for turbulence intensity effects

        2022-01-07 04:33:22ChengXiaoxiang

        Cheng Xiaoxiang

        (School of Civil Engineering, Southeast University, Nanjing 211189, China)

        Abstract:Variations of wind effects on large cooling towers observed at different turbulence intensities for our previous full-scale measurements might be caused by the inherent uncertainties in our physical experiments.Accordingly, the one-way analysis of variance(ANOVA)technique is employed for analyzing the data measured on the prototype Pengcheng cooling tower.Because ANOVA indicates that the variations of full-scale wind effects are basically the effects of turbulence intensity, the empirical results of wind loads on cooling towers obtained by generalizing physical experimental data without considering the turbulence intensity effects are updated using model test results obtained in multiple flow fields.The empirical fluctuating wind pressure distribution is updated based on the fact that the fluctuating wind pressure coefficient linearly increases with the increase in the turbulence intensity, and the empirical formulae of the spectra and the coherences is updated based on conservative assumptions.Comparisons of the empirical results and full-scale measurement data suggest that the original empirical results are either too conservative or unsafe for use.However, economic efficiency and conservativeness will be balanced if the updated empirical results are employed for the wind engineering design.

        Key words:cooling tower; empirical formula; wind tunnel test; full-scale measurement; turbulence intensity

        Research on wind effects on large cooling towers began in the 1970s worldwide[1-5], and the topic of science still receives much attention today[6-11].Our previous research[12-13]proved using quantifiable data that free-stream turbulence significantly influences wind effects on cooling towers.Although the differences in wind loads observed by Cheng et al.[12-13]among different turbulence intensity cases are supposed to result from the discrepancy of the turbulence intensity, we should not disregard that uncertainties in physical experiments can also cause discrepancies.Thus, some effective techniques should be employed to compare the significance of the turbulence intensity with that of the uncertainty in physical experiments.If free-stream turbulence is proven to have a significant influence, then the practice of disregarding the turbulence intensity effects in research and design should be improved.

        Most wind engineering design and research are based on the empirical knowledge obtained by generalizing large quantities of experimental data because physical experiments are usually costly and time-consuming.For wind loads on large cooling towers, empirical formulae are obtained for the mean wind pressure distribution[14], fluctuating wind pressure distribution[15-17], spectra of fluctuating pressures[18], and cross-spectra of fluctuating pressures[19].Some of these empirical formulae[18-19]are obtained by fitting large quantities of experimental data obtained under multiple turbulence intensities, which should be strengthened by considering the turbulence intensity effects for conservativeness.Other empirical formulae are based on full-scale measurements[15-16]or physical model tests with the atmospheric boundary layer(ABL)simulation[17], whose engineering backgrounds are usually cooling towers with heights no greater than 165 m.They are defined by the Chinese standard DL/T 5339—2006[20]as small-sized cooling towers, which are usually located in wind environments with high turbulence intensities.However, cooling towers with heights greater than 165 m are usually subjected to ABL winds with much lower turbulence intensities.In this regard, those formulae based on small-sized cooling towers should also be adjusted to accommodate large cooling tower cases.

        In view of this narrative,in this study, first, the one-way analysis of variance(ANOVA)technique is employed to analyze the significance of the turbulence intensity with our previous full-scale physical experiments[12].Second, based on the calculated significance of the turbulence intensity, an empirical formula updating method that considers the turbulence intensity effects is proposed and presented using a case study.Finally, the effectiveness of the empirical formula updating method is demonstrated by comparing the updated empirical results with the full-scale measurement data.

        1 ANOVA for the Significance of Turbulence Intensity

        1.1 Basic theories

        Some factors might influence the experimental results, and the grades of the factors are called levels.When one factor with more than two levels should be considered for an experiment, one-way ANOVA is a useful practice to analyze the significance of that factor.Supposing that there arerlevels for factor A andnrepetitions of the experiment are conducted for each level, Tab.1 can be obtained.

        Tab.1 Experimental results for one-way ANOVA

        (1)

        (2)

        IfF>Fα(Fαis the critical value corresponding to test levelα), thenH0should be rejected.IfF

        1.2 ANOVA results

        The overviews of the full-scale measurements for wind effects on the prototype Pengcheng cooling tower are previously reported by Cheng et al.[12], which are not repeated here.Using the fluctuating wind pressure coefficients measured at 20° and 80° on the prototype at different turbulence intensities, two ANOVA tables are established(see Tabs.2 and 3).Using data listed in Tab.2, we calculated thatSA=0.089,SE=0.003, andF=133.5.Supposing thatα=0.05,Fα=19.4 is found in the critical value table for the F-test.Accordingly,F>Fαis obtained, which indicates that differences between the data measured at 20° on the prototype are mainly caused by the turbulence intensity effects.Similar results can be obtained by processing the data measured at 80° on the prototype(see Tab.3).In sum, the ANOVA results suggest that the turbulence intensity has a significant influence on the fluctuating wind pressure distribution.

        Tab.2 Fluctuating wind pressure coefficients measured at 20° on the prototype

        Tab.3 Fluctuating wind pressure coefficients measured at 80° on the prototype

        Moreover, according to Ref.[14], the following equation can be utilized to describe the spectra of fluctuating pressures on large cooling towers:

        (3)

        wherenis the frequency anda,b, andcare the parameters possibly depending on the turbulence intensity.The spectra of the fluctuating pressures measured at 20° on the prototype at different turbulence intensities are fitted based on Eq.(3), and the identified parametersa,b, andcin Eq.(3)are listed in Tabs.4 to 6, respectively.Using the data listed in Tab.4, we calculated thatSA=0.278,SE=0.003 06, andF=409.In addition,Fα=19.4 is found in the critical value table withα=0.05.Thus,F>Fαis obtained, which indicates that differences between parameterain Eq.(3)calculated for different time intervals are mainly caused by the turbulence intensity effects.A similar situation also holds true when ANOVA is undertaken for the data listed in Tabs.5 and 6.In this regard, it is proven that turbulence intensity also has a significant influence on the spectra of fluctuating pressures on large cooling towers.

        Tab.4 Identified parameter a for the spectra of fluctuating pressure coefficients measured at 20° on the prototype

        Tab.5 Identified parameter b for the spectra of fluctuating pressure coefficients measured at 20° on the prototype

        Tab.6 Identified parameter c for the spectra of fluctuating pressure coefficients measured at 20° on the prototype

        2 Empirical Results for Wind Pressures on Cooling Towers

        Because the free-stream turbulence is proven to be a significant influence on wind effects on cooling towers in the previous section, the empirical results for wind pressures on cooling towers based on the practice of disregarding the turbulence intensity effects should be improved.In this portion of the study, empirical results for wind effects on cooling towers(i.e., mean and fluctuating wind pressure coefficients, spectra of fluctuating pressures, and coherences between fluctuating pressures)are presented, which will be updated for turbulence intensity effects in the next section.

        2.1 Mean and fluctuating wind pressure coefficients

        According to Ref.[14], the empirical formulae of the proposed mean and fluctuating wind pressure distributions should agree with the obtained full-scale measurement results.A number of investigators have measured the mean and fluctuating wind pressure coefficients on several prototype cooling towers, which are reproduced from Ref.[14], as shown in Fig.1.In Fig.1(a), most mean wind pressure distributions agree well, suggesting that the effects of turbulence intensity on the mean wind pressure coefficients are negligible.Only the values obtained on the Maoming tower appreciably differ from the other sets of values due to the absence of ribs on the external surface of that tower.In Fig.1(b), the agreement between the two fluctuating wind pressure distributions is generally good.The limited discrepancy between the two curves in Fig.1(b)should be the turbulence intensity effects.The results of the empirical formulae for the mean and fluctuating wind pressure distributions are reported by DL/T 5339—2006[20]and Liu[21], respectively.They are also shown in Fig.1, where the empirical formulae of the proposed mean and fluctuating wind pressure distributions agree well with the full-scale measurement results.

        (a)

        2.2 Spectra of fluctuating pressures

        According to Ref.[18], the following expressions can describe the spectra of fluctuating pressures on large cooling towers:

        (4)

        (5)

        (6)

        (7)

        2.3 Coherences between fluctuating pressures

        According to Ref.[19], whenθ≤100°,θ′≤100°, the following expressions can describe the circumferential coherence between fluctuating pressures on large cooling towers:

        (8)

        (9)

        whereθis the included angle between point 1 and the stagnation point;θ′ is the included angle between point 2 and the stagnation point;β3=25;U(δ)is the mean wind speed at the gradient heightδ; andC2(θ,θ′)is given in figures.According to Simiu and Scanlan[14], the coherences between pressures on the windward region(θ≤100°), on the one hand, and pressures on the leeward region(θ′>100°), on the other, are negligible.

        3 Updating Methods for Empirical Results

        According to Cheng et al.[13], free-stream turbulence significantly influences the dynamic characteristics of wind effects on cooling towers.Because the fluctuating wind pressure coefficients around the full half-circle monotonically linearly increase with the increase in turbulence intensity[13], the following equation is employed to update the empirical fluctuating wind pressure distributions measured on small-sized cooling towers with high turbulence intensities(see Fig.1(b)):

        (10)

        whereσp(z1,θ)is the updated fluctuating wind pressure coefficient measured at heightz1circumferential positionθ;σp(z2,θ)is the original fluctuating wind pressure coefficient measured at heightz2; andIu(z1)andIu(z2)are the empirical turbulence intensities for heightz1andz2, respectively.Becausez1>z2,Iu(z1)

        Furthermore,Cheng et al.[13]found that the spectra of fluctuating pressures measured at different positions around the half-circle change irregularly with the increase in turbulence intensity.Because the empirical formulae for the spectra of fluctuating pressures(Eqs.(4)to(7))are obtained by fitting large quantities of experimental data measured in the turbulent flow and laminar flow, Eq.(11)is employed to update the results calculated using the empirical formulae for conservativeness.This condition is based on the fact that the turbulence intensity of the realistic ABL wind approximately varies from zero to the values simulated in conventional ABL wind tunnels[13]:

        Spupd(z,θ,n)=Spemp(z,θ,n)+|Spexp1(z,θ,n)-

        Spexp2(z,θ,n)|

        (11)

        whereSpupd(z,θ,n)andSpemp(z,θ,n)are the updated and original spectrum of the pressure fluctuation at frequencynfor heightzcircumferential positionθ, respectively, andSpexp1(z,θ,n)andSpexp2(z,θ,n)are the spectrum of the pressure fluctuation measured at the same position on the cooling tower model in the wind tunnel with and without the ABL simulation, respectively.Cheng et al.[13]found that a similar situation holds true for coherences between fluctuating pressures(they change irregularly with the increase in turbulence intensity).Accordingly, an equation similar to Eq.(11)is employed to update the results calculated using Eqs.(8)and(9):

        Rfupd(θ,θ′,n)=Rfemp(θ,θ′,n)+|Rfexp1(θ,θ′,n)-

        Rfexp2(θ,θ′,n)|

        (12)

        whereRfupd(θ,θ′,n)is the updated circumferential coherence between fluctuating pressures measured at the circumferential positionθand circumferential positionθ′;Rfemp(θ,θ′,n)is the corresponding original circumferential coherence; andRfexp1(θ,θ′,n)andRfexp2(θ,θ′,n)are the circumferential coherences measured on the cooling tower model in the wind tunnel with and without the ABL simulation, respectively.

        4 Overview of Wind Tunnel Tests

        As mentioned in Section 3, wind tunnel tests with and without the ABL simulation are both required for updating the empirical results of wind loads on cooling towers for turbulence intensity effects.Thus, they are undertaken in the TJ-3 wind tunnel of Tongji University in Shanghai, China.

        The wind tunnel is a closed-circuit rectangular cross-section wind tunnel, wherein the size of the test section is 15 m in width, 2 m in height, and 14 m in length.The test wind speed can be continuously controlled within the 1.0-17.6 m/s range.The non-uniformity of the wind speed of the flow field in the test zone is less than 1%, the turbulence intensity is less than 0.5%, and the average flow deviation angle is less than 0.5°.Using spires and ground roughness blocks(see Fig.2(a)), the ABL turbulent flow field of the countryside open terrain is simulated for the test.Without these passive devices, the laminar flow field is obtained.Based on the scenario of Pengcheng large cooling towers[12], the test model and surroundings are modeled on a geometric scale of 1∶200 using synthetic glass(see Fig.2(b)).The wind tunnel blocking rate is approximately 3% for the test, and the wind tunnel test wind speed is 12 m/s.

        (a)

        36 × 12 taps are arranged on 12 vertical sections and 36 horizontal circular directions for the pressure measuring tower model.DSM3000 electronic pressure scanners from Scanivalve Corp.are used to obtain the wind pressures on the tower surfaces in the laminar flow and ABL turbulent flow.The signal data are acquired at a sample rate of 312.5 Hz, and the sample length is 6 000 data at one tap in each run.By sticking paper belts along the vertical direction and adjusting the incoming flow velocity, the actual static characteristics of the prototype cooling tower at high Reynolds number(Re)are successfully simulated in the reduced-scale model with lowerRe.The turntable rotates from 0° to 360° at 22.5° intervals, but only the case with the same wind direction as that observed in the engineering site of Pengcheng electric power station on Nov.29, 2011 is considered[12].Therefore, the empirical results updated using the model test data can fairly compare with the wind effects measured on the prototype.

        5 Updated Empirical Results and Full-Scale Measurement Data

        Based on the methods described in Section 3, the results presented in Section 2 are updated using the wind tunnel test data.Then, the updated empirical results are compared with the full-scale measurement data obtained on the prototype Pengcheng cooling tower(the field test wind speed is 12.06 m/s at the height of the measurement section)[12].As stated in Section 2.1, the effects of turbulence intensity on the mean wind pressure coefficients are negligible, so only the dynamic empirical results are updated.

        The fluctuating wind pressure distributions measured on the scaled model in the wind tunnel are shown in Fig.3(a).As can be seen, the model test results obtained in the turbulent flow are much greater than those obtained in the laminar flow.Using the discrepancy of the model test data measured in the two flow fields, the two empirical results reported by Ruscheweyh[15]and Sageau[16]are updated following Eq.(10), given that the two empirical results are both obtained at the approximately 90 m height and the full-scale measurement results are obtained at a 130 m height(see Fig.3(b)).The comparison results of the original and updated empirical results with the full-scale data presented in Fig.3(b)clearly indicate that the agreements are better for the updated empirical results than for the original empirical results.Moreover, the updated empirical results are notably different from the full-scale measurement results at certain locations in Fig.3(b), e.g., at 60° and 100°.Although the field measurement data are generally treated as the targets of physical modeling, they might be inaccurate in certain cases, e.g., 1)when the static reference pressure established for the full-scale measurement can hardly play the same role as the static pressure in the wind tunnel and 2)when the full-scale velocity field lacks stationarity and homogeneity.Based on our experiences, the full-scale data presented in Fig.3(b)roughly reflect the trend of fluid physics, but they might not be perfect at certain local points due to the limitations of the field measurement technique.We suppose that the empirical results presented in Fig.3(b)are correct with regard to the fluctuating wind pressure coefficients calculated at 60° and 100°.

        (a)

        Figs.4(a),(c), and(e)show the power spectral densities of fluctuating wind pressures measured at three positions(the subtitles in Fig.4 refer to the included angles between the measurement points and stagnation point)on the scaled model in the wind tunnel.Comparing the result measured in the laminar flow and that measured in the turbulent flow, one can hardly determine which one of them is greater than the other.For conservativeness, the absolute values of the discrepancies between the data measured in the two flow fields are employed for updating the empirical formulae(Eqs.(4)to(7)).The empirical power-spectral densities of the fluctuating wind pressures are updated according to Eq.(11)and compared with the full-scale data, as shown in Figs.4(b),(d), and(f).As shown in Figs.4(b)and(d), the updated empirical results are accurate for use, and it might be unsafe to directly utilize the original empirical formulae(Eqs.(4)to(7)).In particular, the updating practice is better for results calculated at the windward side(see Figs.4(b)and(d))than for results calculated at the leeward side(see Fig.4(f)).This condition is probably because the fluid physics is quite different at different locations.Therefore, the unified updating practice to all locations might lead to a certain inaccuracy.The corresponding revision of the unified updating practice is being undertaken by the authors now.However, due to the limited article length, this topic will be reported in another article.

        (a)

        Figs.5(a),(c), and(e)describe the effects of turbulence intensity on the coherences between the wind pressure coefficient samples obtained at 20° and other positions on the scaled model in the wind tunnel.Because it is difficult to tell whether the free-stream turbulence can strengthen or reduce the coherences, Eq.(12)also relies on the absolute values of the discrepancies between data measured in the two flow fields to update the empirical results.The updated empirical coherences are also compared with the full-scale data in Figs.5(b),(d), and(f), which suggests that the updated empirical results are slightly conservative for use.

        6 Conclusions

        1)The one-way ANOVA technique is employed to analyze the influence of the turbulence intensity on our previous full-scale measurement data.The results clearly indicate that the variations of wind effects measured on the prototype Pengcheng cooling tower are basically the effects of turbulence intensity rather than the effects of the inherent uncertainties in our physical experiments.

        (a)

        2)The comparison of the empirical results of wind loads on cooling towers with the corresponding full-scale measurement data shows that the empirical fluctuating wind pressure distributions are too conservative for use.Although the frequency-domain empirical formulae may lead to unsafe structural designs, the practice of generalizing empirical results of wind loads on cooling towers from physical experimental data, which disregards the turbulence intensity effects, is improved.

        3)Updating methods for the empirical results of wind loads on cooling towers for turbulence intensity effects are formulated.The comparisons of the updated empirical results and full-scale measurement data suggest that economic efficiency and conservativeness will be balanced if the updated empirical results are employed for the wind engineering design.

        91精品国产乱码久久久| 激情 一区二区| 久久国产精品99精品国产987| 东京热加勒比日韩精品| 操老熟妇老女人一区二区| av网站不卡的av在线| 人妻少妇无乱码中文字幕| 精品人妻一区二区三区视频| 午夜久久久久久禁播电影| 国产精品中文久久久久久久| 欧美国产一区二区三区激情无套| 最近高清中文在线字幕观看| 亚洲av无码一区二区乱子仑| 男男互吃大丁视频网站| 视频区一区二在线观看| 十八禁视频网站在线观看| 久久露脸国产精品| 精品久久综合亚洲伊人| 不卡a v无码在线| 色婷婷av一区二区三区丝袜美腿| 色吧噜噜一区二区三区| 偷国产乱人伦偷精品视频| 伊人久久五月丁香综合中文亚洲 | 国产精品18久久久久久麻辣| 香色肉欲色综合| 亚洲av午夜福利精品一区二区| 成人国产av精品麻豆网址| 久久午夜精品人妻一区二区三区| 麻豆精品国产精华液好用吗| 人妻少妇邻居少妇好多水在线| 国产色噜噜| 国产优质女主播在线观看| 在线观看麻豆精品视频| av无码国产在线看免费网站| 黑人大荫道bbwbbb高潮潮喷| 亚洲一区二区自拍偷拍| 综合图区亚洲偷自拍熟女| 日本护士口爆吞精视频| 亚洲熟女www一区二区三区 | 亚洲av永久无码精品三区在线 | 亚洲熟妇在线视频观看|